Credit
Vitaly Kuzmin · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
MiG-31 · Length
Single source22.62 m (74 ft 3 in)[source]
Length
Single sourceConfiguration
| Specification | Mikoyan MiG-31 | Sukhoi Su-33 |
|---|---|---|
| Type | Interceptor aircraft , strike fighter[source] | Carrier-based air superiority fighter with multirole capabilities[source] |
| National origin | Soviet Union[source] | Soviet Union Russia[source] |
| Manufacturer | Mikoyan-Gurevich/Mikoyan[source] | Sukhoi , Komsomolsk-on-Amur Aircraft Production Association[source] |
| Status | In service with the Russian Air Force[source] | In service |
21.19 m (69 ft 6 in)[source]
wing folded
Single source7.40 m (24 ft 3 in) wing folded[source]
Empty; MiG-31 · Empty weight
Single sourceGross; MiG-31 · Gross weight
Single sourceMaximum take-off; MiG-31 · Max takeoff weight
Single source21,820 kg (48,105 lb)[source]
41,000 kg (90,390 lb)[source]
46,200 kg (101,854 lb)[source]
Empty; Empty weight
Single sourceGross; Gross weight
Single sourceCruise; MiG-31 · / Mach 2.35
Single sourceMaximum; MiG-31 · / Mach 2.83 at 21,500 m (70,500 ft)
Single source3,000 km/h (1,900 mph, 1,600 kn) / Mach 2.83 at 21,500 m (70,500 ft)[source]
2,500 km/h (1,600 mph, 1,300 kn) / Mach 2.35[source]
Maximum; at 10,000 m (33,000 ft)
Single source2,300 km/h (1,430 mph, 1,240 kn) at 10,000 m (33,000 ft)[source]
MiG-31 · at Mach 0.8 and
Single sourceMiG-31 · Combat range
Single source1,450 km (900 mi, 780 nmi) at Mach 0.8 and 10,000 m (33,000 ft)[source]
MiG-31 · 2 × Soloviev D-30 F6 afterburning turbofan engines thrust each dry
Single sourceMiG-31 · with afterburner
Single source2 × Soloviev D-30 F6 afterburning turbofan engines, 93 kN (21,000 lbf) thrust each dry, 152 kN (34,000 lbf) with afterburner[source]
2 × Saturn AL-31F3 afterburning turbofan engines thrust each dry
Single sourcewith afterburner
Single sourceBars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | Russian Aerospace Forces Kazakh Air Defense Forces (historical)[source] | — |
|---|
| Number built | 519[source] | 24 built total[source] |
|---|
| Manufactured | 1975–1994[source] | 1987–1999[source] |
|---|
| Introduction date | 6 May 1981[source] | 31 August 1998 (official)[source] |
|---|
| First flight | 16 September 1975 ( 1975-09-16 )[source] | 17 August 1987 ( 1987-08-17 )[source] |
|---|
| Retired | 2023 (Kazakh Air Force)[source] | — |
|---|
| Developed from | Mikoyan-Gurevich MiG-25[source] | Sukhoi Su-27[source] |
|---|
| Fuel capacity | 35,550 lb (16,130 kg) internals, plus optional external fuel tanks[source] | 9,500 kg (20,900 lb) internal[source] |
|---|
| Guns | 1 × 23 mm Gryazev-Shipunov GSh-6-23 M rotary cannon with 260 rounds.[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds[source] |
|---|
| Hardpoints | 4 × semi-recessed under the fuselage and 4 × underwing pylons with capacity of up to 9,000 kg (20,000 lb) of ordnance , with provisions to carry combinations of: Missiles: Air-to-air missiles : 4 × R-33 2 × R-40 RD/TD 4 × R-60 MK 4 × R-73 4 × R-77 4 × R-37 M (MiG-31BM only) 4 × R-77 M (MiG-31BM only)[source] | 12 × external hardpoints with a capacity of up to 6,500 kg (14,300 lb) of ordnance, with provisions to carry combinations of: Rockets: S-8 KOM/BM/OM S-13 T/OF S-25 OFM-PU Missiles: Air-to-air missiles : 8 × R-27 R/ER/T/ET 4 × R-73 E Anti-ship missiles : Kh-31 A Kh-41 Anti-radiation missiles : Kh-25 MP Kh-31 P Bombs: RBK-500 cluster bomb Up to 500 kg (1,100 lb) bombs[source] |
|---|
| g limits | 5+[source] | + 8[source] |
|---|
| Wing loading | 665 kg/m 2 (136 lb/sq ft)[source] | 483 kg/m 2 (99 lb/sq ft)[source] |
|---|
| Thrust/weight | 0.85[source] | 0.83[source] |
|---|
| Missiles | Air-to-air missiles :[source] | Air-to-air missiles : 8 × R-27 R/ER/T/ET 4 × R-73 E Anti-ship missiles : Kh-31 A Kh-41 Anti-radiation missiles : Kh-25 MP Kh-31 P[source] |
|---|
| Primary user | — | Russian Navy[source] |
|---|
| Variant | — | Shenyang J-15[source] |
|---|
| Stall speed | — | 240 km/h (150 mph, 130 kn)[source] |
|---|
| Landing speed | — | 240 km/h (150 mph; 130 kn)[source] |
|---|
| Rockets | — | S-8 KOM/BM/OM S-13 T/OF S-25 OFM-PU[source] |
|---|
| Bombs | — | RBK-500 cluster bomb Up to 500 kg (1,100 lb) bombs[source] |
|---|
Maximum take-off; Max takeoff weight
2 × Saturn AL-31F3 afterburning turbofan engines, 74.5 kN (16,700 lbf) thrust each dry, 125.5 kN (28,200 lbf) with afterburner[source]